Simulated Air Launch Environment. Volume 1

Abstract

A program was conducted in which the response and failure characteristics of solid propellant rocket motors when subjected to transient thermal conditions representing air launch operational environments were recorded and analyzed. Future Air Force mission profiles were used. The Maverick motor, AGM-65A, was used as a test bed on the program.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1974
Accession Number
ADB001103

Entities

People

  • O. R. Pritts

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Climate Change
  • Failure Mode And Effect Analysis
  • Geometry
  • Heat Transfer
  • Low Temperature
  • Mechanics
  • Physical Properties
  • Stress Strain Relations
  • Temperature Gradients
  • Tensile Properties
  • Test And Evaluation
  • Test Facilities
  • Test Methods
  • Thermal Conductivity
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Missile Defense Systems.
  • Software Engineering
  • Thermal Physics or Thermal Science.